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The unit takes a byte command and outputs a sequence with the command repeated, roll, pitch and yaw coded in floating point radians, a system time stamp and a checksum. The standard API for windows includes all the command parsing sections except the serial communication bits. As usual to test the stability of the unit I did a static run. The attitude stability is indeed 1° peak-to-peak. The graphs show some high frequency noise, the flight control needs to perform some smoothing and rounding to deal with that.
Here is the version of the Linux sample ported from the 3DM-GX1 Linux sample provided by Microstrain.
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